搜索资源列表
sldemo_f14
- This demonstration models a flight control for the longitudinal motion of a Grumman Aerospace F-14 Tomcat. First order linear approximations of the aircraft and actuator behavior are connected to an analog flight control design that uses the pilot
GestureApp
- VC开发的鼠标姿势识别软件,使用了SVM向量机算法.-A program of mouse attitude recognise,use the SVM arithmetic to realize.
chzf.rar
- 惯性导航系统中求解航向及姿态角的仿真程序，用matlab开发,Inertial navigation system to solve direction and attitude angle of the simulation program, developed by matlab
INS_OUT2
- 捷联惯性导航技术中使用四元数算法实现姿态更新矩阵的求解，得到姿态角。-Strapdown inertial navigation technology using quaternion attitude update algorithm for solving the matrix, get attitude angle.
EKF
- 卫星姿态确定的卡尔曼滤波，使用matlab 仿真的姿态确定-satellite attitude determination
dcmfromeulerang
- 飞行器姿态角的欧拉角表示方法与余弦矩阵表示方法的matlab转换程序-Aircraft attitude angle of the Euler angle method with cosine matrix methods matlab conversion process
201003tecplot
- 简介卫星姿态控制系统的模型，并针对该模型分析故障发生的特点，故 障诊断的难点，以及可能发生故障的部位和故障的类型，给出故障检测的方法。-Introduction of satellite attitude control system model and the model for the analysis of the characteristics of faults, fault diagnosis of the difficulties, and possible failure l
Attitude-Control-of-Spinning-Satellite
- simulate multivariable system control. Attitude Control of Spinning Satellite Subject to Actuators Restriction Using EigenStructure Assignment.
Attitude-SINS
- 姿态角仿真 MATLAB 捷联惯导 三阶泰勒 四阶龙格库塔-MATLAB simulation Attitude SINS fourth order Runge-Kutta third-order Taylor
Missile-Attitude-control
- 1、利用simulink中sfunction方法建立航天器姿态动力学模型和运动学模型； 2、利用linmod对非线性模型线性化； 3、姿态模型线性化后，利用极点配置（pole）方法求取控制参数； 4、将控制参数带入非线性模型仿真控制效果。-One using simulink sfunction method to establish the dynamic model and kinematic model of the spacecraft attitude 2,
Attitude-solving-operator-program
- 物体姿态解算算法子程序，包涵了各种在姿态解算仿真是需要用到的子程序，-The object attitude solution to calculate another way the program encompasses a variety of attitude solution simulation is the need to use a subroutine,
attitude-determinati-
- 多GPS天线姿态确定程序，包括文件读取、单点定位、双差定位、坐标转换以及姿态确定等。-a MATLAB toolbox for determining the attitude of a rigid platform by means of multiple non-dedicated antennas using global positioning system is presented. The programs embedded in this toolbox cover t
Satellite-attitude-control-model
- 卫星姿态控制模型 用于控制算法的验证和仿真-Satellite attitude control model
MEMS-attitude-estimation
- 一篇关于AHRS动态姿态解算的好文章，英文题目A Robust Nonlinear Observer for Real-Time Attitude Estimation Using Low-Cost MEMS Inertial Sensors-An excellent article about AHRS attitude dynamic solver, the English title A Robust Nonlinear Observer for Real-Time Attitude Es
spacecraft-attitude-quaternion
- 对航天器的姿态以四元数的方法建立的仿真模型 。对航天器进行建模-The simulation model for spacecraft attitude quaternion method established. Spacecraft modeling
Attitude-arithmetic-forSTM21
- MPU6050+HMC5883+STM32平衡小车，姿态解算MCU源代码，串口发送。这个可以用IMU软件查看数据变化情况。-MPU6050+ HMC5883+ STM32 balanced car, attitude solution MCU source code and serial port. This software can be used to view the data changes IMU.
Satellite-attitude-control-system
- 自动控制理论中卫星姿态控制系统，利用MATLAB画出已校正系统的单位阶跃和单位斜坡响应曲线。-The satellite attitude control system of automatic control theory is used to draw the unit step and slope response curve of the corrected system with MATLAB.
Fourth - order runge-kutta
- 惯性测量元件输出的传感器数据，利用四阶龙格库计算姿态(caculator attitude in Fourth - order runge-kutta)
attitude control of satellite
- attitude control of satellite with principal axes
实验代码
- 卫星姿态控制仿真，包括卫星轨道建模、卫星运动学、动力学建模，跟踪律计算(Satellite attitude control simulation, including satellite orbit modeling, satellite kinematics, dynamic modeling, tracking law calculation)